Abstract: An oxygen container for a passenger transport vehicle with a compartment configured to hold at least one oxygen mask, a moving mount coupled to the compartment and configured to linearly or pivotally move the compartment from a stowed position to a release position, and a bottom lid hinged to the compartment and configured to move to an open position and releasing the at least one oxygen mask, when the compartment moves from the stowed position to the release position. Also provided are a monument and a passenger vehicle section, as well as an aircraft having such an oxygen container.

Abstract: A vehicle region with a roof section of a primary structure and with two luggage compartments. One of the luggage compartments comprises a detachable luggage compartment flap and a luggage compartment top, which forms the upper boundary of a part of a luggage space. A detachable fastening device can rotatably fasten the luggage compartment flap on the luggage compartment. A front edge of the luggage compartment top is at a distance from an end point in an intermediate space above a luggage compartment, to which end point a side of a ceiling panel is movable, the distance being greater than or equal to a width of the ceiling panel. Methods for installing and removing a ceiling panel above two luggage compartments are provided, wherein the ceiling panel is guided at least partially through a luggage space of a luggage compartment when the luggage compartment flap has been removed.

Abstract: An aircraft cabin arrangement is disclosed which extends in a rectilinear manner along a cabin axis, having a ceiling trim arrangement which delimits the cabin interior upwardly from the cabin axis, wherein the ceiling trim arrangement has a first, a second and a third row of ceiling trim elements, wherein the rows are arranged one immediately after another in the direction of extent of the cabin axis, wherein the rows have a central ceiling trim element and lateral ceiling trim elements, wherein the lateral ceiling trim elements of a row immediately adjoin the central ceiling trim element of the row in a laterally adjacent manner on both sides, perpendicularly to the cabin axis, wherein the lateral ceiling trim elements of the second row have one or more lighting sources, wherein the axial lengths of the ceiling trim elements of the first and the third row are different.

Abstract: A process for manufacturing a vehicle cabin part (1) to fit in a gap (9) between a first component (5) and a second component (7) including: providing different sealing bodies (3?) each having a first lateral face (11?) conforming to an inner surface (17?) of the first component (5?) and a second lateral face (13?) spaced a certain distance (15?) from the first lateral face (11?); select one of the sealing bodies having a certain distance that fits the gap (9) between the first component (5) and the second component (7); insert the selected sealing body (3) into the gap (9) such that the first lateral face (11) at least partially adjoins the inner surface (17) of the first component (5) and the second lateral face (13) at least partially adjoins the outer surface (21) of the second component (7) facing the first component (5).

Abstract: A ceiling trim element for a passenger cabin of a vehicle, in particular for an aircraft cabin of an aircraft which has a planar panel element with a front side and a rear side, wherein the front side is provided to point towards the interior of the passenger cabin, and the rear side is provided to point away from the interior of the passenger cabin, wherein an image surface is provided in the panel element, wherein the image surface is assigned a varying pattern generator in order to illuminate the image surface with varying patterns, and having an illuminating ring generator to generate an illuminating ring which surrounds the image surface.

Abstract: A passenger cabin area, which is suitable for installation in an aircraft cabin, includes passenger seats arranged one behind another along a longitudinal axis of the passenger cabin area. The passenger cabin area also includes luggage compartments which are arranged, at least in certain sections, in an area between an inner face, which faces towards an interior space of the passenger cabin area, of a fuselage sidewall and the passenger seats, and have an access aperture which faces towards the passenger seats.

Abstract: A passenger cabin area, which is suitable for installation in an aircraft cabin, includes passenger seats arranged one behind another along a longitudinal axis of the passenger cabin area. The passenger cabin area also includes luggage compartments which are arranged, at least in certain sections, in an area between an inner face, which faces towards an interior space of the passenger cabin area, of a fuselage sidewall and the passenger seats, and have an access aperture which faces towards the passenger seats.

Abstract: A passenger seat arrangement comprises at least one first seat arranged at a first lower level, and at least one second seat arranged at a second elevated level. Each of the first and the second seats comprises a supporting surface for supporting a passenger which is movable between an upright seating position and a reclined lying position. At least one of the first and the second seats is constructed in such a manner that a movement of its supporting surface from the upright seating position into the reclined lying position results in an increase of a distance between the supporting surface of the first seat and the supporting surface of the second seat.

Abstract: An interior trim arrangement for an aircraft cabin, having lateral ceiling elements, and an angled element having limbs limb extending from one another, one lateral ceiling element arranged offset upwardly and to a first side, the angled element arranged with the first limb adjoining a lateral ceiling element towards the first side, the free end of the first limb located opposite the free end, towards the first side, of a lateral ceiling element, the other limb extending towards the other lateral ceiling element, the free end of the second limb spaced apart from the first free end, towards a lateral ceiling element, of the other lateral ceiling element, a light source for the other lateral ceiling element between the free end of the second limb and the first free end, towards a lateral ceiling element, of the other lateral ceiling element, and the angled element having a lighting element.

Abstract: An aircraft cabin arrangement for a passenger aircraft, extending along a cabin axis which runs centrally through the aircraft cabin arrangement, having a ceiling trim arrangement provided in the upwardly pointing part of the outer wall of the aircraft cabin arrangement and is arranged above the cabin axis, wherein the ceiling trim arrangement comprises a central ceiling panel element and lateral ceiling panel elements which have a panel element, wherein the central ceiling panel element is arranged vertically above the cabin axis, wherein the lateral ceiling panel elements adjoin the central ceiling panel element on both sides in the lateral direction perpendicularly with respect to the cabin axis, wherein one or more of the central ceiling panel element and the lateral ceiling panel elements has a flat lighting device which is embodied in a flat fashion such that it extends over a surface section of the ceiling panel element.

Abstract: A process for manufacturing a vehicle cabin part (1) to fit in a gap (9) between a first component (5) and a second component (7) including: providing different sealing bodies (3?) each having a first lateral face (11?) conforming to an inner surface (17?) of the first component (5?) and a second lateral face (13?) spaced a certain distance (15?) from the first lateral face (11?); select one of the sealing bodies having a certain distance that fits the gap (9) between the first component (5) and the second component (7); insert the selected sealing body (3) into the gap (9) such that the first lateral face (11) at least partially adjoins the inner surface (17) of the first component (5) and the second lateral face (13) at least partially adjoins the outer surface (21) of the second component (7) facing the first component (5).

Abstract: A crew rest compartment for a means of transport includes a first bunk and a second bunk, wherein the first bunk is located above the second bunk. Each bunk includes a sleeping area for accommodating a sleeping crew member, wherein each sleeping area has a longitudinal direction. The first bunk is aligned such that the longitudinal direction of the first bunk and a longitudinal direction of the crew rest compartment enclose an angle which differs from 0° and 90°.

Abstract: An aircraft cabin arrangement for a passenger aircraft, extending along a cabin axis which runs centrally through the aircraft cabin arrangement, having a ceiling trim arrangement provided in the upwardly pointing part of the outer wall of the aircraft cabin arrangement and is arranged above the cabin axis, wherein the ceiling trim arrangement comprises a central ceiling panel element and lateral ceiling panel elements which have a panel element, wherein the central ceiling panel element is arranged vertically above the cabin axis, wherein the lateral ceiling panel elements adjoin the central ceiling panel element on both sides in the lateral direction perpendicularly with respect to the cabin axis, wherein one or more of the central ceiling panel element and the lateral ceiling panel elements has a flat lighting device which is embodied in a flat fashion such that it extends over a surface section of the ceiling panel element.

Abstract: An aircraft cabin arrangement is disclosed which extends in a rectilinear manner along a cabin axis, having a ceiling trim arrangement which delimits the cabin interior upwardly from the cabin axis, wherein the ceiling trim arrangement has a first, a second and a third row of ceiling trim elements, wherein the rows are arranged one immediately after another in the direction of extent of the cabin axis, wherein the rows have a central ceiling trim element and lateral ceiling trim elements, wherein the lateral ceiling trim elements of a row immediately adjoin the central ceiling trim element of the row in a laterally adjacent manner on both sides, perpendicularly to the cabin axis, wherein the lateral ceiling trim elements of the second row have one or more lighting sources, wherein the axial lengths of the ceiling trim elements of the first and the third row are different.

Abstract: A ceiling trim element for a passenger cabin of a vehicle, in particular for an aircraft cabin of an aircraft which has a planar panel element with a front side and a rear side, wherein the front side is provided to point towards the interior of the passenger cabin, and the rear side is provided to point away from the interior of the passenger cabin, wherein an image surface is provided in the panel element, wherein the image surface is assigned a varying pattern generator in order to illuminate the image surface with varying patterns, and having an illuminating ring generator to generate an illuminating ring which surrounds the image surface.

Abstract: An interior trim arrangement for an aircraft cabin, having lateral ceiling elements, and an angled element having limbs limb extending from one another, one lateral ceiling element arranged offset upwardly and to a first side, the angled element arranged with the first limb adjoining a lateral ceiling element towards the first side, the free end of the first limb located opposite the free end, towards the first side, of a lateral ceiling element, the other limb extending towards the other lateral ceiling element, the free end of the second limb spaced apart from the first free end, towards a lateral ceiling element, of the other lateral ceiling element, a light source for the other lateral ceiling element between the free end of the second limb and the first free end, towards a lateral ceiling element, of the other lateral ceiling element, and the angled element having a lighting element.

Abstract: A crew rest compartment for a means of transport includes a first bunk and a second bunk, wherein the first bunk is located above the second bunk. Each bunk includes a sleeping area for accommodating a sleeping crew member, wherein each sleeping area has a longitudinal direction. The first bunk is aligned such that the longitudinal direction of the first bunk and a longitudinal direction of the crew rest compartment enclose an angle which differs from 0° and 90°.